Fault-tolerant permanent magnet machine with reconfigurable stator core slot opening and back iron flux paths

ABSTRACT

A permanent magnet (PM) machine includes a plurality of reconfigurable fault condition mechanisms disposed within a stator core portion, the plurality of reconfigurable fault condition mechanisms together automatically reconfigurable to reduce fault currents and internal heat associated with the PM machine during a fault condition. The plurality of reconfigurable fault condition mechanisms are disposed solely within the stator core portion according to one embodiment to automatically reduce stator winding fault currents and internal heat associated with the PM machine during a fault condition. A method of reconfiguring the fault condition mechanisms upon detecting a fault condition includes the steps of 1) selecting the plurality of reconfigurable fault condition mechanisms from a) a plurality of rotatable magnetically anisotropic cylinders disposed both within a stator back iron and stator slot openings, and b) a plurality of rotatable magnetically anisotropic cylinders disposed within a stator back iron and a sliding shield disposed with a stator slot opening portion of the stator core, and 2) reconfiguring the plurality of fault condition mechanisms together to automatically reduce fault currents associated with the PM machine upon detection of a fault condition.

BACKGROUND

The present invention is directed to permanent magnet machines, and more particularly to a method of making a permanent magnet machine more fault-tolerant.

Many new aircraft systems are designed to accommodate electrical loads that are greater than those on current aircraft systems. The electrical system specifications of commercial airliner designs currently being developed may demand up to twice the electrical power of current commercial airliners. This increased electrical power demand must be derived from mechanical power extracted from the engines that power the aircraft. When operating an aircraft engine at relatively low power levels, e.g., while idly descending from altitude, extracting this additional electrical power from the engine mechanical power may reduce the ability to operate the engine properly.

Traditionally, electrical power is extracted from the high-pressure (HP) engine spool in a gas turbine engine. The relatively high operating speed of the HP engine spool makes it an ideal source of mechanical power to drive the electrical generators connected to the engine. However, it is desirable to draw power from additional sources within the engine, rather than rely solely on the HP engine spool to drive the electrical generators. The low-pressure (LP) engine spool provides an alternate source of power transfer.

PM machines (or generators) are a possible means for extracting electric power from the LP spool. However, aviation applications require fault tolerance, and as discussed below, PM machines can experience faults under certain circumstances and existing techniques for fault tolerant PM generators suffer from drawbacks, such as increased size and weight.

Permanent magnet (PM) machines have high power and torque density. Using PM machines in applications wherein minimizing the weight is a critical factor is therefore advantageous. These applications are wide ranging and include aerospace applications.

One of the key concerns with using PM machines is fault-tolerance since the magnets cannot be “turned off” in case of a fault. Traditionally, the use of PM machines has been avoided in applications where fault-tolerance is a key factor. When PM machines have been used in such applications, fault-tolerance has been achieved by paying a penalty in the form of oversized machines and/or converter designs, or using a higher number of phases which complicates the control process and adds to the overall system weight and cost.

As is known to those skilled in the art, electrical generators may utilize permanent magnets (PM) as a primary mechanism to generate magnetic fields of high magnitudes. Such machines, also termed PM machines, are formed from other electrical and mechanical components, such as wiring or windings, shafts, bearings and so forth, enabling the conversion of electrical energy from mechanical energy, where in the case of electrical motors the converse is true. Unlike electromagnets which can be controlled, e.g., turned on and off, by electrical energy, PMs always remain on, that is, magnetic fields produced by the PM persists due to their inherent ferromagnetic properties. Consequently, should an electrical device having a PM experience a fault, it may not be possible to expediently stop the device because of the persistent magnetic field of the PM causing the device to keep operating. Such faults may be in the form of fault currents produced due to defects in the stator windings or mechanical faults arising from defective or worn-out mechanical components disposed within the device. Hence, the inability to control the PM during the above mentioned or other related faults may damage the PM machine and/or devices coupled thereto.

Further, fault-tolerant systems currently used in PM machines substantially increase the size and weight of these devices limiting the scope of applications in which such PM machines can be employed. Moreover, such fault tolerant systems require cumbersome designs of complicated control systems, substantially increasing the cost of the PM machine.

In view of the foregoing, it would be advantageous and beneficial to provide a method for limiting winding currents for all types of faults, especially a turn-to-turn fault associated with a PM machine to significantly improve the fault-tolerance capability of the PM machine without substantially increasing the size, weight and/or complexity of the PM machine.

BRIEF DESCRIPTION OF THE INVENTION

The present invention is directed to a permanent magnet (PM) machine comprising a plurality of reconfigurable fault condition mechanisms disposed within a stator core portion, the plurality of reconfigurable fault condition mechanisms together automatically reconfigurable to reduce fault currents and internal heat associated with the PM machine during a fault condition.

The plurality of reconfigurable fault condition mechanisms are disposed solely within the stator core portion according to one embodiment to automatically reduce stator winding fault currents and internal heat associated with the PM machine during a fault condition.

A method of reconfiguring the fault condition mechanisms upon detecting a fault condition comprises the steps of 1) selecting the plurality of reconfigurable fault condition mechanisms from a) a plurality of rotatable magnetically anisotropic cylinders disposed both within a stator back iron and stator slot openings, and b) a plurality of rotatable magnetically anisotropic cylinders disposed within a stator back iron and a sliding shield disposed with a stator slot opening portion of the stator core, and 2) reconfiguring the plurality of fault condition mechanisms together to automatically reduce fault currents associated with the PM machine upon detection of a fault condition.

BRIEF DESCRIPTION OF THE DRAWINGS

Other aspects and features of the present invention and many of the attendant advantages of the present invention will be readily appreciated as the same become better understood by reference to the following detailed description when considered in connection with the accompanying drawings in which like reference numerals designate like parts throughout the figures thereof and wherein:

FIG. 1 illustrates a portion of a permanent magnet (PM) machine depicting rotatable anisotropic material cylinders in the PM machine stator core slots as well as the stator slot openings under normal operating conditions according to one embodiment of the present invention;

FIG. 2 illustrates a portion of a permanent magnet (PM) machine depicting rotatable anisotropic material cylinders in the PM machine stator core slots as well as the stator slot openings under a fault condition according to one embodiment of the present invention;

FIGS. 3 a and 3 b illustrate an actuator or gear assembly for rotating the rotatable cylinders shown in FIGS. 1 and 2.

FIG. 4 illustrates portion of a permanent magnet (PM) machine depicting rotatable anisotropic material cylinders in the stator back iron and a sliding shield having magnetic and non-magnetic sections in the PM machine stator slot side during normal operating conditions according to one embodiment of the present invention;

FIG. 5 illustrates portion of a permanent magnet (PM) machine depicting rotatable anisotropic material cylinders in the stator back iron and a sliding shield having magnetic and non-magnetic sections in the PM machine stator slot side during a fault condition according to one embodiment of the present invention;

FIG. 6 is a block diagram illustrating a general provision for protection of a permanent magnet generator using active and/or passive detection of a thermal overload condition and triggering a protection mechanism actuator according to one embodiment of the present invention; and

FIG. 7 illustrates a conventional permanent magnet machine architecture that is known in the prior art.

While the above-identified drawing figures set forth alternative embodiments, other embodiments of the present invention are also contemplated, as noted in the discussion. In all cases, this disclosure presents illustrated embodiments of the present invention by way of representation and not limitation. Numerous other modifications and embodiments can be devised by those skilled in the art which fall within the scope and spirit of the principles of this invention.

DETAILED DESCRIPTION

Conventional PM synchronous electric machines employ permanent magnets as the magnetic poles of a rotor, around which a stator is disposed. The stator has a plurality of teeth that face the rotor. Alternatively, the machine may be designed so that the rotor surrounds the stator. For high-speed operation, a retaining sleeve is usually wrapped around the magnets as needed to keep the magnets in place. The retaining sleeve may be shrink fit upon the magnets to ensure a non-slip fit. Usually the retaining sleeve is made of one whole metallic piece for structural integrity. When the coils formed on the stator are energized, a magnetic flux is induced by the current through the coils, creating electromagnetic forces between the stator and the rotor. These electromagnetic forces contain tangential and/or circumferential forces that cause the rotor to rotate.

In order to achieve inherent fault-tolerance in these PM machines, there has to be complete electromagnetic, thermal, and physical isolation between the coils of the various phases. This is achieved by using fractional-slot concentrated windings where each coil is wound around a single stator tooth and each stator slot is occupied by one side of a coil. Since slots formed between the teeth and the permanent magnets on the rotor are spaced from each other, the magnetic flux passing through a tooth will pass through the neighboring tooth in the next moment as the rotor rotates.

The fault-tolerance techniques discussed herein are not limited to PM machines with fractional-slot concentrated windings. They can just as easily be applied to any PM machine with any winding configuration to achieve the desired results.

A conventional PM machine that is known in the art is shown in FIG. 7 to provide a background regarding PM machine architecture before describing several embodiments for implementing a synchronous permanent magnet machine that is fault-tolerant, and with particular focus on turn-to-turn faults, with reference to FIGS. 1-6 herein below.

As can be seen in FIG. 7, a PM machine 1 contains a plurality of magnets 2 provided in a radial arrangement upon a back iron 3 that is disposed around a shaft (not shown). The back iron 3 is also known as a yoke. The magnets 2 are surrounded by a retaining sleeve 4. A stator 5 surrounds the retaining sleeve 4 and is separated from the magnets 2 by a gap 6. The stator 5 has a plurality of radially disposed teeth 7 that form stator slots 8. The teeth 7 are wound with coils 9 that substantially fill the stator slots 8.

Looking now at FIGS. 1 and 2, there is shown, a portion of a permanent magnet machine depicting rotatable cylinders 10. The rotatable cylinders 10 are constructed of a magnetically anisotropic material. Each magnetically anisotropic cylinder can be implemented by forming the cylinder from, for example, a magnetically anisotropic material or from a plurality of magnetic laminations. These laminations can be, for example, any grade of silicon-steel laminations (e.g., M19, M23, . . . , etc.) or any grade of iron-cobalt laminations. The magnetically anisotropic rotatable cylinders 10 are located both in permanent magnet machine stator core slot openings 12 of the stator core 14 as well as a stator back iron 11 according to one embodiment of the present invention. The orientation of the magnetically anisotropic material or magnetic laminations then either impedes or allows a flux path through the slot openings 12 or through the stator back iron (yoke) 11. The rotatable magnetically anisotropic (laminated magnetic) cylinders 10 can be seen in FIG. 1 to be oriented in a direction to conduct a normal magnetic flux path 16 through the stator core back iron (yoke) 11 under normal operating conditions. Under fault conditions, all rotatable magnetically anisotropic cylinders 10 are rotated to simultaneously impede or interrupt the normal magnetic flux path 16 in the stator back iron 11 and allow a flux path through the slot openings 12.

FIG. 2 depicts the new flux path 18 under a fault condition and shows the new flux path 18 does not pass through the back iron 11 of the permanent magnet machine. The rotatable anisotropic cylinders 10 in the stator back iron 11 are disengaged to block the normal flux path (orthogonal to the flux path) 16. In this manner, the rotatable anisotropic cylinders 10 in the stator core slots 12 are rotated 90° under fault conditions to allow a flux path through the slot openings and thus reduce the magnetic flux coupling the stator windings and limit the fault current.

FIGS. 3 a and 3 b illustrate actuation of the rotatable anisotropic cylinders 10 depicted in FIGS. 1 and 2. Rotation of the rotatable anisotropic cylinders 10 is implemented via an actuator or gear assembly 20. The actuator or gear assembly 20 is affixed on permanent magnet machine end plates (not shown) in one embodiment. Many types of actuators and gear assemblies suitable for implementing this structure are easily constructed by those skilled in mechanical engineering; and so actuators and gear assemblies are not discussed in any detail herein to preserve brevity and provide clarity in describing the particular embodiments herein. Under normal operation, the rotatable magnetically anisotropic cylinders 10 in the stator back iron 11 are engaged, while the rotatable magnetically anisotropic cylinders 10 in the stator slot openings 12 are disengaged to provide a normal flux path 16 through the back iron 11 such as depicted in FIG. 1.

During a fault condition, the rotatable magnetically anisotropic cylinders 10 in the stator back iron 11 are disengaged; while the rotatable magnetically anisotropic cylinders 10 in the stator slot openings 12 are engaged by the actuator or gear assembly 20 as seen in FIGS. 3 a and 3 b, to rotate the rotatable anisotropic cylinders 10 by approximately 90° to impede or block the normal flux path 16, thereby shunting the magnetic flux away from the windings via a new flux path 18 as shown in FIG. 2, and reducing the fault currents.

FIGS. 4 and 5 illustrate a sliding shield 45 in the stator slot opening side of a permanent magnet (PM) machine stator core 14. Sliding shield 45 has magnetic sections 52 and nonmagnetic sections 54. In one embodiment, a plurality of axial-laminated portions are inserted, with solid pieces of nonmagnetic material inserted between each laminated portion. The laminated portions can be constructed, for example, using the same, but not limited to, materials used for the rotatable magnetically anisotropic cylinders. The sliding shield 45, according to one embodiment, can be made of a dual-phase magnetic material where the nonmagnetic sections are heat treated. The magnetic sections can also be constructed, for example, of a magnetically anisotropic material or can optionally be constructed of magnetic laminations. During normal operation as shown in FIG. 4, the sliding shield 45 is in its conventional operating mode in which the nonmagnetic sections 54 are aligned to impede a flux path through the stator core slot openings 12 and thus allow flux to pass through the normal flux path 16 through the stator back iron 11.

With continued reference to FIGS. 4 and 5, stator core 14 can be seen to also have a plurality of rotatable cylinders such as discussed herein before with reference to FIGS. 1 and 2, disposed within the back iron 11. As shown in FIG. 4, the sliding shield 45 is positioned such that the nonmagnetic sections 54 are aligned with the slot openings 12 during normal fault-free operation to impede a flux path through the slot openings 12; while the rotatable cylinders 10 are rotated to conduct a flux path through the back iron 11 during fault-free operation.

FIG. 5 illustrates the sliding shield 45 and the rotatable cylinders 10 during a fault condition in which the sliding shield 45 is positioned such that the magnetic material sections 52 are aligned with and provide a flux path through the slot openings 12, while the rotatable cylinders 10 in the back iron 11 are rotated to impede the flux path through the back iron 11. The magnetically anisotropic material may optionally be replaced with laminated magnetic portions, as stated herein before.

If a localized electrical fault occurs in the stator core 14 of the permanent magnet machine, excitation provided by the permanent magnet rotor 21 can cause significant overload current to flow, as described herein before. Localized heating will occur in this case. When the foregoing localized heating occurs, the heat generated at the internal stator core 14 fault will be detected via an active or passive thermal overload detector mechanism such as described further herein below with reference to FIG. 6. The thermal overload detector mechanism will then activate movement of the sliding shield 45 such that the magnetic sections 52 now create a shunt across the stator core slot openings 12 to divert more flux through flux path 18 through the stator core slot openings 12, and less flux through the normal flux path through the stator back iron 11 thus reduce the magnetic flux coupling with the stator windings and limit the fault current. In similar fashion, the thermal overload detector mechanism will activate rotation of the cylinders 10 in the back iron 11 to provide a flux path during normal fault-free operation. The thermal overload detector mechanism will then reorient the rotatable cylinders 10 during a fault condition to impede a flux path through the back iron 11.

FIG. 6 is a block diagram illustrating a permanent magnet machine (i.e. generator) 50 using active and/or passive detection of a thermal overload condition, and triggering a protection mechanism actuator 20 according to one embodiment of the present invention. The permanent magnet machine 50 is controlled in response to commands from a generator controller 53 that senses one or more loads 55 supplied by the machine 50. The generator controller 53 is also in communication with an active thermal overload detection system 56 that operates to sense operating point conditions that are conducive to machine 50 overloading. Many types of active thermal overload detection methods and systems suitable for implementing the requisite active thermal overload detection system 56 are known in the art, and so further details of thermal overload detection systems will not be discussed herein.

When the active thermal overload detection system 56 detects an operating condition that exceeds one or more desired or predetermined operating condition set points, the active thermal overload detection system 56 sends one or more command signals to the protective mechanism actuator 20. The protective mechanism actuator 20 then operates in response to the command signal(s) to operate the rotatable cylinders 10 and the sliding shield 45 shown in FIGS. 1-2 and 4-5 respectively as described herein before.

With continued reference now to FIG. 6, a passive thermal overload detection system (sensor) 60 is configured to directly sense thermal conditions of the permanent magnet machine (generator) 50. When the passive thermal overload detection system 60 is subjected to an operating condition that exceeds one or more desired or predetermined operating condition set points, the passive thermal overload detection system 60 physical state is altered. This changed physical state is detected by the protective mechanism actuator 20. The protective mechanism actuator 20 then operates in response to the altered physical state to operate the rotatable cylinders 10 and the sliding shield 45 shown in FIGS. 1-2 and 4-5 respectively as described herein before.

In summary explanation, methods for improving the fault-tolerance of PM machines have been described to include various electrical, mechanical, hydraulic or thermal solutions that provide flexibility in choosing the optimal PM machine architecture from a system point of view. These solutions include, but are not limited to 1) rotatable anisotropic or laminated magnetic cylinders 10 in the stator core slot openings 12 to interrupt the stator flux through the stator back iron 11 under fault conditions, 2) a sliding shield in the stator core slot opening side that operates to impede a flux path through the stator back iron 11 under fault conditions, and 3) combining desired features described above as necessary to achieve desired system performance, reliability, cost, size, specifications/requirements, and so on.

A key feature of the embodiments described herein before include the provision of a fault tolerant permanent magnet machine that is more robust than permanent magnet machines known in the art that employ more conventional types of fault sensing mechanisms, actuators, controllers, and so on.

While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims. 

1. A permanent magnet (PM) machine comprising: a stator core portion; a rotor core portion; and a plurality of reconfigurable fault condition mechanisms disposed solely within the stator core portion, the plurality of reconfigurable fault condition mechanisms together automatically reconfigurable to reduce fault currents and internal heat associated with the PM machine during a fault condition.
 2. The PM machine according to claim 1, wherein the plurality of fault condition mechanisms comprise a plurality of rotatable cylinders comprising anisotropic material or magnetic laminations disposed both within stator slot openings and a stator back iron of the stator core portion.
 3. The PM machine according to claim 2 further comprising an actuator or gear assembly configured to rotate the plurality of rotatable cylinders during a PM machine fault condition.
 4. The PM machine according to claim 3, wherein the actuator or gear assembly is responsive to electrical signals generated via an active thermal overload detector.
 5. The PM machine according to claim 3, wherein the actuator or gear assembly is responsive to electrical signals generated via a passive thermal overload detector.
 6. The PM machine according to claim 2, wherein the rotatable cylinders are oriented during normal PM machine operation to conduct a flux path through the stator back iron and impede a flux path through the stator slot openings.
 7. The PM machine according to claim 2, wherein the rotatable cylinders are oriented during a PM machine fault condition to impede a flux path through the stator back iron and conduct a flux path through the stator slot openings.
 8. The PM machine according to claim 1, wherein the plurality of fault condition mechanisms comprise a plurality of rotatable cylinders comprising anisotropic material or magnetic laminations disposed within a stator back iron and a sliding shield disposed within a slot opening portion of the stator core portion.
 9. The PM machine according to claim 8 further comprising an actuator or gear assembly configured to rotate the plurality of rotatable cylinders and move the sliding shield during a PM machine fault condition.
 10. The PM machine according to claim 9, wherein the actuator or gear assembly is responsive to electrical signals generated via an active thermal overload detector.
 11. The PM machine according to claim 9, wherein the actuator or gear assembly is responsive to electrical signals generated via a passive thermal overload detector.
 12. The PM machine according to claim 8, wherein the rotatable cylinders are oriented during normal fault-free PM machine operation to conduct a flux path through the stator back iron, and further wherein the sliding shield is moved during normal fault-free PM machine operation to impede a flux path through stator slot openings.
 13. The PM machine according to claim 8, wherein the rotatable cylinders are oriented during a PM machine fault condition to impede a flux path through the stator back iron, and further wherein the sliding shield is moved during a PM machine fault condition to conduct a flux path through stator slot openings.
 14. A permanent magnet (PM) machine comprising a stator portion having a plurality of fault condition mechanisms disposed therein, the plurality of fault condition mechanisms automatically reconfigurable in combination to reduce stator winding fault currents and internal heat associated with the PM machine during a fault condition.
 15. The PM machine according to claim 14, wherein the plurality of fault condition mechanisms comprises at least one rotatable cylinder disposed within a back iron of the stator portion, and further comprises a sliding shield disposed within a stator slot opening portion of the stator portion.
 16. The PM machine according to claim 15, wherein the sliding shield comprises a plurality of sections selected from a dual-phase magnetic material, magnetic laminations, and magnetically anisotropic material.
 17. The PM machine according to claim 15, wherein the at least one rotatable cylinder is constructed of magnetically anisotropic material.
 18. The PM machine according to claim 15, wherein the at least one rotatable cylinder is oriented during normal fault-free PM machine operation to conduct a flux path through the stator back iron, and further wherein the sliding shield is positioned during normal fault-free PM machine operation to impede a flux path through stator slot openings.
 19. The PM machine according to claim 14 further comprising an actuator or gear assembly configured to rotate the at least one rotatable cylinder and move the sliding shield during a PM machine fault condition.
 20. The PM machine according to claim 19, wherein the actuator or gear assembly is responsive to electrical signals generated via an active thermal overload detector.
 21. The PM machine according to claim 19, wherein the actuator or gear assembly is responsive to changed physical condition associated with a passive thermal overload detector.
 22. A method of reconfiguring a permanent magnet (PM) machine upon detecting a fault condition, the method comprising the steps of: providing permanent magnet (PM) machine with a stator core comprising a plurality of fault condition mechanisms disposed therein, the plurality of mechanisms selected from a plurality of rotatable magnetically anisotropic cylinders disposed both within a stator back iron and stator slot openings, and a plurality of rotatable magnetically anisotropic cylinders disposed within a stator back iron and a sliding shield disposed with a stator slot opening portion of the stator core; and reconfiguring the plurality of fault condition mechanisms together to automatically reduce fault currents associated with the PM machine upon detection of a fault condition.
 23. The method according to claim 22, wherein the step of reconfiguring the plurality of fault condition mechanisms comprises rotating the plurality of magnetically anisotropic cylinders, such that the plurality of magnetically anisotropic cylinders impede a normal PM machine flux path through a back iron of the stator core, and moving the sliding shield to conduct a flux path through the stator core slots.
 24. The method according to claim 22, wherein the step of reconfiguring the plurality of fault condition mechanisms comprises rotating the plurality of magnetically anisotropic cylinders such that the magnetically anisotropic cylinders in the back iron impede a flux path through a back iron of the stator core, and further such that the magnetically anisotropic cylinders in the stator slots conduct a flux path through the stator core slots. 